首页> 美国政府科技报告 >Free-flight measurements of the rolling effectiveness and operating characteristics of a bellows-actuated split-flap aileron on a 60 degree delta wing at Mach numbers between 0.8 and 1.8

【24h】

Free-flight measurements of the rolling effectiveness and operating characteristics of a bellows-actuated split-flap aileron on a 60 degree delta wing at Mach numbers between 0.8 and 1.8

机译：自由飞行测量波纹管驱动的分瓣式副翼在60度三角翼上的马达数在0.8到1.8之间的滚动效率和操作特性

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

No Abstract Available

著录项

作者
Schult, Eugene D;
展开▼
作者单位

展开▼
年度 1954
页码 1-35
总页数 35
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词

相似文献

外文文献

1. Experimental Investigation of Vortex Flow over an 80 Degree/60 Degree Double Delta Wing at Sideslip [J] . G. Atashbaz, M. Ommian Journal of Aircraft . 2006,第3期

机译：侧滑80度/ 60度双三角翼涡流的实验研究
2. Time-History Effects on a Rolling 65-Degree Delta-Wing-Body Configuration [J] . Lars E. Ericsson Journal of Aircraft . 1999,第3期

机译：滚动65度Delta-Wing-Body配置的时间历史效应
3. UNSTEADY AERODYNAMIC CHARACTERISTICS ON ROLLING DELTA WINGS [J] . KWAK DONG YOUN 日本航空宇宙学会論文集 . 1999,第543期

机译：轧制三角翼上的非定常气动特性
4. Modelling of the Nonlinear Lift and Pitching Moment Characteristics of 60 Degrees Delta Wing and Wing- bodies [C] . M. Rajamurthy AIAA Guidance, Navigation, and Control Conference and Exhibit . 2002

机译：60度三角翼和翼身非线性升力和俯仰力矩特性的建模
5. Modeling the rolling moment on the 65-degree delta wing for rolling motions at high angle of attack. [D] . Myatt, James Harold. 1997

机译：对65度三角翼上的侧倾力矩进行建模，以实现高攻角下的侧倾运动。
6. Low speed aerodynamic characteristics of 60 degrees rounded leading-edge delta wing with vortex flaps [O] . Rinoie K. 1996

机译：带有涡流襟翼的60度圆形前缘三角翼的低速空气动力学特性

Free-flight measurements of the rolling effectiveness and operating characteristics of a bellows-actuated split-flap aileron on a 60 degree delta wing at Mach numbers between 0.8 and 1.8

摘要

著录项

相似文献

相关主题

期刊订阅